Optimal Control Design of Slow Dominant Transient Response for Longitudinal Missile Dynamics-Reference-Cited by-同舟云学术

Optimal Control Design of Slow Dominant Transient Response for Longitudinal Missile Dynamics

Published:2023-10-26 Issue: Volume: Page:
ISSN:
Container-title:2023 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology (ICARES)
language:
Short-container-title:

Author:

Putro Idris E.¹,Subiantoro Aries¹,Halim Abdul¹,Triharjanto Robertus H.²,Syafiie S.³

Affiliation:

1. Universitas Indonesia,Dept. of Electrical Engineering,Depok,Indonesia

2. National Research and Innovation Agency (BRIN),Research Organization for Aeronautics and Space (ORPA),Jakarta,Indonesia

3. Faculty of Engineering-Rabigh, King AbdulAziz University,Dept. of Chemical and Materials Engineering,Jeddah,Saudi Arabia

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10329884/10329790/10329801.pdf?arnumber=10329801

Reference23 articles.

1. Analysis of optimal midcourse guidance law

2. Missile Guidance and Control Systems

3. Simulation and Analysis of Integral LQR Controller for Inner Control Loop Design of a Fixed Wing Micro Aerial Vehicle (MAV)

4. Application of Explicit/Model Following Control Technology in The Attitude Control System for The Unmanned Shipboard Helicopter;Tao;Journal of Naval Aeronautical Engineering Institute,2009

5. Optimization as a support for selection and design of aircraft actuation systems

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Controllability Analysis of Longitudinal Canard-based Sounding Rocket Dynamics at Certain Flight Conditions;2023 7th International Conference on Electrical, Telecommunication and Computer Engineering (ELTICOM);2023-12-13